Airbus A321-211

Service difficulty reports · 12,330

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A321211'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAA2013011100009Shear Plate · corroded2S CHECK. SHEAR PLATE IS CORRODED AT -Y1589 BETWEEN FR 69 AND FR 70. REMOVED AND REPLACED SHEAR PLATE IAW TR 320-2528-10-0011E.Dec 31, 2012 · N190UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011100004Cleat · corroded2S CHECK - FUSELAGE FRAME TO SKIN CLEAT CORRODED AT FR 41 BETWEEN S40R AND S41R. REMOVED AND REPLACED CLEAT IAW A321 SRM 51-72-11 AND AIRBUS DRAWING D53234411.Dec 31, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013010900023Floor Support · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR64 TO FR65, Y765. REPLACED FLOOR SUPPORT BEAM BETWEEN FR64 TO FR65, Y765 IAW A321 SRM 51-42-11 & AIRBUS DRAWING 18D53472815.Dec 31, 2012 · N190UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013010200006Bottle · low pressureFORWARD FLIGHT ATTENDANT ANNUNCIATOR PANEL "CHECK DOOR 3L PRESSURE". SERVICED 3L DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.Dec 31, 2012 · N196UW · Airbus A321211 · Emergency ExitsSDR USAA2012122800008Actuator · defectiveCREW DECLARED AN EMERGENCY ON APPROACH DUE TO SLATS 1 AND 2 MALFUNCTION - BOTH FAILED TO EXTEND. MAINTENANCE COULD NOT DUPLICATE FAULT. INSPECTED LEFT/RIGHT WING SLAT ROTARY ACTUATORS. REPLACED RIGHT WING NR 4 SLAT INBOARD ROTARY ACTUATOR (6087CM) DUE TO TRDec 26, 2012 · N169UW · Airbus A321211 · Leading Edge Slat ActuatorSDR USAA2012122700001Bottle · low pressureCIDS PANEL CAUTION LIGHT ILLUMINATED DURING BOARDING PROCESS. MAINTENANCE FOUND 2R DOOR BOTTLE PRESSURE LOW - SERVICED 2R DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.Dec 25, 2012 · N186US · Airbus A321211 · Emergency ExitsSDR USAA2012122400024Lens · brokenEMERGENCY EXIT LIGHT COVER BROKEN OFF SEAT 10C. REPLACED LENS.Dec 23, 2012 · N176UW · Airbus A321211 · Emergency LightingSDR USAA2012122400023Connector · looseEMERGENCY EXIT LIGHT (RED) AT L-3 DOOR RIGHT SIDE INOPERATIVE. FOUND CONNECTOR LOOSE AT SIDEWALL. RECONNECTED CONNECTOR. OPERATIONAL CHECK GOOD.Dec 23, 2012 · N193UW · Airbus A321211 · Light System WiringSDR USAA2013010400011Splice Plate · cracked2S CHECK - CRACK IN CROSS BEAM CONNECTING SECTION AT FR68, S23L. REPLACED CROSS BEAM CONNECTING SECTION AT FR68, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53474250.Dec 21, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2012122800013Mechanism · out of tolerance2S CHECK - OUT OF ADJUSTMENT STRIKER LEVER MEASURE DIMENSION ON DOOR DAMPER MECHANISM AT PASSENGER/CREW DOOR 842. PERFORMED ADJUSTMENT OF THE FINGER OF THE PERCUSSION BELL CRANK IN THE X AXIS & CHECKED CLEARANCES J2 OR DIMENSION A BETWEEN FINGER AND STRIKER LDec 21, 2012 · N165US · Airbus A321211 · Passenger/Crew DoorsSDR USAA2012122800012Mechanism · out of tolerance2S CHECK - OUT OF ADJUST STRIKER LEVER MEASURE DIMENSION A ON DOOR DAMPER MECHANISM AT PASSENGER/CREW DOOR 832. PERFORMED ADJUSTMENT OF THE FINGER OF THE PERCUSSION BELLCRANK IN THE X AXIS & CHECKED CLEARANCES J2 OR DIMENSION A BETWEEN FINGER AND STRIKER LEVERDec 20, 2012 · N165US · Airbus A321211 · Passenger/Crew DoorsSDR USAA2012122800002Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER SHAPE SILL BETWEEN FR66 TO FR68, S23R. REPLACED CENTER SHAPE SILL BETWEEN FR66 TO FR68, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480505.Dec 20, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2012122100012Lens · missingEMERGENCY LIGHT LENS MISSING AT REAR RIGHT OF AFT GALLEY. MAINTENANCE REPLACED LENS.Dec 20, 2012 · N182UW · Airbus A321211 · Emergency LightingSDR USAA2012122100010Reservoir · low pressureCIDS CAUTION 'SLIDE PRESS LOW MID LEFT'. REMOVED AND REPLACED L2 SLIDE BOTTLE IAW AIRBUS MAINTENANCE MANUAL 25-62-49.Dec 20, 2012 · N162UW · Airbus A321211 · Escape SlideSDR USAA2012122100008Cylinder · low pressureCIDS CAUTION LIGHT ON FLIGHT ATTENDANT PANEL DOOR PRESSURE LOW MID RIGHT. SERVICED MID RIGHT DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002A.Dec 20, 2012 · N162UW · Airbus A321211 · Emergency ExitsSDR USAA2013011500029Access Panel · damaged2S CHECK - ELONGATED HOLES ON LEFT WING LOWER FUEL DOOR 540HB BETWEEN WS 7316 TO WS 7792, BETWEEN S8L TO S11L & BETWEEN RIB 13 TO RIB 14 . REPLACED LEFT WING LOWER FUEL DOOR 540HB IAW A321 SRM 57-27-11 & AMM 57-27-11-400-001-A.Dec 19, 2012 · N165US · Airbus A321211 · Wing, Plate/SkinSDR USAA2013011000027Fitting · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON LOWER SILL CENTER FITTING BETWEEN FR16 TO FR20, S23L. REPLACED LOWER SILL CENTER FITTING BETWEEN FR16 TO FR20, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112198 & D53112109.Dec 17, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2012121800002Seal · leakingA HAZE AND STRONG CHEMICAL ODOR WERE PRESENT IN THE CABIN WITH APU BLEED ON. CREW MEMBER REPORTED BURNING EYES AND THROAT IRRITATION. ODOR DISSIPATED WITH APU BLEED AIR OFF. MAINTENANCE REMOVED AND REPLACED THE APU. HONEYWELL CONFIRMED THE FAILURE OF THE LODec 15, 2012 · N167US · Airbus A321211 · APU Core EngineSDR USAA2013010800026Hinge Fitting · worn2S CHECK - WEAR ON NR 6 ELEVATOR HINGE FITTING ON RIGHT HORIZONTAL STABILIZER AT STAB STA 5894, THS RIB 13. REPLACED NR 6 ELEVATOR HINGE FITTING ON RIGHT HORIZONTAL STABILIZER AT STAB STA 5894, THS RIB 13 IAW A321 AMM 55-16-42.Dec 15, 2012 · N165US · Airbus A321211 · Elevator StructureSDR USAA2013010800025Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON HINGE FITTING NR 3 ON RIGHT HORIZONTAL STABILIZER AT STAB STA 297, THS RIB 8. REPLACED RIGHT HORIZONTAL STABILIZER NR 3 HINGE FITTING AT STAB STA 297, THS RIB 8 IAW A321 AMM 55-16-42.Dec 15, 2012 · N165US · Airbus A321211 · Horizontal Stabilizer StructureSDR USAA2013011700028Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR47.5+5 INCHES, Y765. REPLACED SEAT RAIL AT FR47.5+5 INCHES, Y765 IAW A321 SRM 51-72-11.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011700027Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR55+10 INCHES, Y765. REPLACED SEAT RAIL AT FR55+10 INCHES, Y765 IAW A321 SRM 53-41-15 PARAGRAPH 5B, FIGURE 202.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011700026Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47.5 TO FR63, -Y1292. REPLACED SEAT RAIL BETWEEN FR47.5 TO FR63, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472650.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011500026Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR63 TO FR64, -Y1292. REPLACED SEAT RAIL BETWEEN FR63 TO FR64, -Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472817.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011000028Fitting · corroded2S CHECK - LEVEL 2 FILIFORM CORROSION ON CENTER FITTING AT LOWER CUT-OUT OF RIGHT FORWARD PASSENGER/CREW DOOR WAY BETWEEN FR16 TO FR20, S23R. REPLACED CENTER FITTING BETWEEN FR16 TO FR20, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53112109.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013010800027Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR68, S23L. REPLACED CORNER FITTING AT FR68, S23L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480505.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013010400013Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT L2 DOOR ENTRYWAY BETWEEN FR66 TO FR68, S23L, Y1732. REPLACED CENTER FITTING AT L2 DOOR ENTRYWAY BETWEEN FR66 TO FR68, S23L, Y1732 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480505.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013010400012Fitting · corroded2S CHECK - LEVEL 2 INTERGRANULAR CORROSION ON AFT CORNER FITTING AT R2 DOOR ENTRYWAY AT FR68, S23R. REPLACED AFT CORNER FITTING AT R2 DOOR ENTRYWAY AT FR68, S23R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53480505.Dec 14, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011500024Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACKS BETWEEN FR24 TO FR35, -Y765. REPLACED SEAT TRACKS BETWEEN FR24 TO FR35, -Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234433.Dec 13, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011100005Stringer · corroded2S CHECK - STRINGER CORRODED AT S43L BETWEEN FR 64 AND FR 66. REPAIRED STRINGER IAW A321 SRM 53-00-13 FIG 201 (SHEET 2).Dec 13, 2012 · N165US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013012200016Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR41+8 INCHES, -Y1292. REPLACED SHEAR PLATE BETWEEN FR47.2A TO FR47.4, S28R IAW A321 SRM 51-72-11, EA 503688 & AIRBUS DRAWING D53372500.Dec 12, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011500025Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACKS BETWEEN FR41 TO FR47, Y765. REPLACED SEAT TRACKS BETWEEN FR41 TO FR47, Y765 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53372500 & D53371110.Dec 12, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013012200017Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN S40R TO S41R. REPLACED CLEAT AT FR30 BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011700033Stringer · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STRINGER AT FR33+1 INCHES, S41R. REPAIRED STRINGER BETWEEN FR31+1 INCHES TO FR33+1 INCHES, S41R IAW A321 SRM 53-21-13.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Main, Longeron/StringerSDR USAA2013011700032Plate · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON PLATE AT DME NR 2 ANTENNA BETWEEN FR24 TO FR24A & BETWEEN S43R TO S44. REPLACED PLATE AT DME NR 2 ANTENNA BETWEEN FR24 TO FR24A & BETWEEN S43R TO S44 IAW A321 SRM 51-72-11.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011700025Shear Tie · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE (CLEAT) AT FR33 BETWEEN S40R TO S41R. REPLACED SHEAR TIE (CLEAT) AT FR33 BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA2013011700024Shear Tie · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE (CLEAT) AT FR31 BETWEEN S41R TO S42R. REPLACED SHEAR TIE (CLEAT) AT FR31 BETWEEN S41R TO S42R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA2013011700023Shear Tie · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE (CLEAT) AT FR34 BETWEEN S40R TO S41R. REPLACED SHEAR TIE (CLEAT) AT FR34 BETWEEN S40R TO S41R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA2013011700022Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR27 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR27 BETWEEN S41R TO S42R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011500030Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY AT NR 7 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 569/BR7. REPLACED NR 7 RUDDER HINGE FITTING AT VERTICAL STABILIZER STA 569/BR7 IAW A321 SRM 51-72-11 & AMM 55-36-41.Dec 11, 2012 · N165US · Airbus A321211 · Rudder StructureSDR USAA2013011500018Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR35.4 BETWEEN S42L TO S43L. REPLACED CLEAT AT FR35.4 BETWEEN S42L TO S43L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53235030.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011500017Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR26 BETWEEN S42L TO S43L. REPLACED CLEAT AT FR26 BETWEEN S42L TO S43L IAW A321 SRM 51-72-11.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011500016Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR28 BETWEEN S42R TO S43R. REPLACED CLEAT AT FR28 BETWEEN S42R TO S43R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011500014Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR32 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR32 BETWEEN S41R TO S42R IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234411.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011500013Shear Tie · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR28 BETWEEN S42L TO S43L. REPLACED CLEAT (SHEAR TIE) AT FR28 BETWEEN S42L TO S43L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA2013011000031Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR65+19 INCHES, Y1732. REPLACED FLOORBEAM AT FR65+19 INCHES, Y1732 IAW A321 SRM 51-72-11, AIRBUS DRAWING D53474250 & D53472750.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013011000030Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY AT FR65+18 INCHES, -Y465. REPLACED FLOORBEAM ASSEMBLY AT FR65+18 INCHES, -Y465 IAW A321 SRM 51-72-11 & AIRBUS DRAWING # D53472816.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013011000013Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR64 TO FR66, Y1292. REPLACED SEAT RAIL BETWEEN FR64 TO FR66, Y1292 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013011000009Shear Tie · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR26 BETWEEN S43R TO S43L. REPLACED CLEAT (SHEAR TIE) AT FR26 BETWEEN S43R TO S43L IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53234615.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage Internal Mounting StructureSDR USAA2013010400018Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM BETWEEN FR64 TO FR66, Y765. REPLACED SEAT RAIL BEAM BETWEEN FR64 TO FR66, Y765 IAW A321 SRM 51-72-11 & AIRBUS DRAWING D53472815.Dec 11, 2012 · N165US · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings
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